| 发明名称 | Combustor probe for gas turbine | ||
| 摘要 | Embodiments of the present disclosure are directed towards a turbine combustor probe having a combustion dynamics monitoring probe configured to monitor combustion dynamics within a turbine combustor. The turbine combustor probe also has a gas sampling sleeve configured to collect a gas sample from an airflow path between a liner and a flow sleeve of the turbine combustor. | ||
| 申请公布号 | US8997558(B2) | 申请公布日期 | 2015.04.07 |
| 申请号 | US201113075055 | 申请日期 | 2011.03.29 |
| 申请人 | General Electric Company | 发明人 | Romig Bryan Wesley;Kegley Jonathan Hale;Clifford Robert Wade;Simons Derrick Walter |
| 分类号 | G01M15/05;G01N1/22;F01D21/00 | 主分类号 | G01M15/05 |
| 代理机构 | Fletcher Yoder, P.C. | 代理人 | Fletcher Yoder, P.C. |
| 主权项 | 1. A system, comprising: a turbine combustor; a combustor probe, comprising: a combustion dynamics monitoring probe configured to monitor combustion dynamics within the turbine combustor; anda gas sampling sleeve disposed about the combustion dynamics monitoring probe and configured to collect a gas sample from an airflow path between a liner and a flow sleeve of the turbine combustor; anda combustor probe holder configured to mount the combustor probe within a probe port of the flow sleeve; and a gas monitoring system coupled to the gas sampling sleeve, wherein the gas monitoring system is configured to receive and analyze the gas sample. | ||
| 地址 | Schenectady NY US | ||